GOE 570 AIRFOIL (goe570-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 570 AIRFOIL (goe570-il) Reynolds number: 1,000,000 Max Cl/Cd: 20.85 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe570-il-1000000.txt Download as CSV file: xf-goe570-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 570 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.0704 0.05717 0.05209 -0.2303 0.7339 0.0523
-19.500 -0.0717 0.05480 0.04965 -0.2315 0.7292 0.0529
-19.250 -0.0677 0.05311 0.04789 -0.2320 0.7248 0.0529
-19.000 -0.0654 0.05131 0.04601 -0.2325 0.7203 0.0531
-18.750 -0.0610 0.04960 0.04426 -0.2331 0.7174 0.0532
-18.500 -0.0568 0.04797 0.04259 -0.2335 0.7143 0.0533
-18.250 -0.0549 0.04604 0.04060 -0.2343 0.7108 0.0539
-18.000 -0.0484 0.04481 0.03930 -0.2342 0.7070 0.0537
-17.750 -0.0446 0.04333 0.03775 -0.2343 0.7030 0.0539
-17.500 -0.0392 0.04185 0.03622 -0.2346 0.6997 0.0542
-17.250 -0.0355 0.04030 0.03463 -0.2348 0.6972 0.0544
-17.000 -0.0272 0.03924 0.03355 -0.2345 0.6943 0.0543
-16.750 -0.0228 0.03788 0.03213 -0.2344 0.6912 0.0545
-16.500 -0.0173 0.03670 0.03090 -0.2341 0.6877 0.0547
-16.250 -0.0117 0.03566 0.02979 -0.2334 0.6837 0.0547
-16.000 -0.0039 0.03461 0.02868 -0.2331 0.6801 0.0547
-15.750 0.0017 0.03347 0.02753 -0.2326 0.6779 0.0548
-15.500 0.0075 0.03243 0.02647 -0.2318 0.6748 0.0549
-15.250 0.0119 0.03138 0.02538 -0.2308 0.6716 0.0551
-15.000 0.0161 0.03042 0.02437 -0.2296 0.6681 0.0552
-14.750 0.0203 0.02953 0.02343 -0.2283 0.6644 0.0552
-14.500 0.0221 0.02853 0.02237 -0.2268 0.6602 0.0554
-14.250 0.0221 0.02741 0.02124 -0.2251 0.6580 0.0557
-14.000 0.0222 0.02633 0.02016 -0.2233 0.6552 0.0561
-13.750 0.0235 0.02543 0.01923 -0.2214 0.6515 0.0562
-13.500 0.0199 0.02457 0.01832 -0.2185 0.6474 0.0564
-13.250 0.0160 0.02386 0.01755 -0.2153 0.6429 0.0564
-13.000 0.0136 0.02305 0.01671 -0.2124 0.6393 0.0565
-12.750 0.0129 0.02229 0.01594 -0.2097 0.6363 0.0568
-12.500 0.0136 0.02167 0.01530 -0.2069 0.6323 0.0572
-12.250 0.0102 0.02105 0.01463 -0.2033 0.6279 0.0571
-12.000 0.0050 0.02052 0.01404 -0.1992 0.6232 0.0573
-11.750 0.0041 0.02002 0.01351 -0.1957 0.6193 0.0574
-11.500 0.0040 0.01957 0.01304 -0.1922 0.6151 0.0578
-11.250 -0.0018 0.01918 0.01262 -0.1875 0.6102 0.0579
-11.000 -0.0113 0.01890 0.01227 -0.1819 0.6052 0.0581
-10.750 -0.0166 0.01859 0.01192 -0.1770 0.6008 0.0582
-10.500 -0.0164 0.01830 0.01161 -0.1730 0.5967 0.0584
-10.250 -0.0206 0.01805 0.01132 -0.1680 0.5918 0.0585
-10.000 -0.0291 0.01793 0.01115 -0.1621 0.5864 0.0588
-9.750 -0.0371 0.01777 0.01095 -0.1563 0.5818 0.0590
-9.500 -0.0375 0.01759 0.01075 -0.1518 0.5775 0.0593
-9.250 -0.0437 0.01748 0.01059 -0.1462 0.5722 0.0593
-9.000 -0.0540 0.01746 0.01052 -0.1397 0.5671 0.0595
-8.750 -0.0576 0.01739 0.01040 -0.1344 0.5629 0.0598
-8.500 -0.0598 0.01731 0.01030 -0.1294 0.5587 0.0600
-8.250 -0.0650 0.01728 0.01024 -0.1237 0.5545 0.0601
-8.000 -0.0717 0.01731 0.01021 -0.1178 0.5499 0.0603
-7.750 -0.0803 0.01740 0.01025 -0.1115 0.5453 0.0605
-7.500 -0.0771 0.01736 0.01020 -0.1073 0.5423 0.0607
-7.250 -0.0761 0.01739 0.01020 -0.1027 0.5384 0.0608
-7.000 -0.0802 0.01740 0.01017 -0.0973 0.5346 0.0612
-6.750 -0.0856 0.01747 0.01019 -0.0916 0.5298 0.0617
-6.500 -0.0869 0.01753 0.01022 -0.0867 0.5262 0.0622
-6.250 -0.0808 0.01751 0.01020 -0.0830 0.5235 0.0628
-6.000 -0.0754 0.01753 0.01020 -0.0792 0.5201 0.0634
-5.750 -0.0724 0.01765 0.01030 -0.0751 0.5167 0.0638
-5.500 -0.0706 0.01782 0.01043 -0.0708 0.5129 0.0640
-5.250 -0.0669 0.01799 0.01055 -0.0668 0.5085 0.0649
-5.000 -0.0564 0.01803 0.01060 -0.0640 0.5061 0.0655
-4.750 -0.0474 0.01814 0.01070 -0.0610 0.5035 0.0661
-4.500 -0.0375 0.01827 0.01081 -0.0582 0.5005 0.0664
-4.250 -0.0280 0.01843 0.01093 -0.0553 0.4974 0.0674
-4.000 -0.0228 0.01865 0.01112 -0.0518 0.4935 0.0687
-3.750 -0.0130 0.01883 0.01128 -0.0491 0.4901 0.0697
-3.500 0.0025 0.01891 0.01139 -0.0474 0.4882 0.0718
-3.250 0.0185 0.01902 0.01151 -0.0458 0.4859 0.0735
-3.000 0.0340 0.01914 0.01164 -0.0442 0.4832 0.0765
-2.750 0.0454 0.01941 0.01191 -0.0420 0.4798 0.0795
-2.500 0.0573 0.01969 0.01219 -0.0399 0.4765 0.0833
-2.250 0.0712 0.01990 0.01240 -0.0382 0.4725 0.0918
-2.000 0.0903 0.02001 0.01257 -0.0373 0.4708 0.1008
-1.750 0.1081 0.02015 0.01279 -0.0364 0.4687 0.1147
-1.500 0.1276 0.02012 0.01302 -0.0359 0.4665 0.1651
-1.250 0.1450 0.02040 0.01336 -0.0349 0.4637 0.1810
-1.000 0.1613 0.02074 0.01371 -0.0338 0.4608 0.1891
-0.750 0.1736 0.02124 0.01420 -0.0321 0.4573 0.1946
-0.500 0.1896 0.02165 0.01456 -0.0309 0.4540 0.1983
-0.250 0.2089 0.02194 0.01489 -0.0304 0.4523 0.2032
0.000 0.2287 0.02223 0.01522 -0.0299 0.4504 0.2085
0.250 0.2469 0.02260 0.01559 -0.0292 0.4480 0.2115
0.500 0.2622 0.02310 0.01608 -0.0281 0.4453 0.2138
0.750 0.2779 0.02359 0.01654 -0.0271 0.4428 0.2156
1.000 0.2924 0.02411 0.01703 -0.0260 0.4395 0.2192
1.250 0.3110 0.02446 0.01737 -0.0254 0.4364 0.2244
1.500 0.3278 0.02496 0.01792 -0.0247 0.4348 0.2282
1.750 0.3458 0.02541 0.01840 -0.0242 0.4328 0.2320
2.000 0.3640 0.02588 0.01886 -0.0237 0.4305 0.2351
2.250 0.3825 0.02629 0.01932 -0.0234 0.4283 0.2452
2.500 0.3974 0.02690 0.01992 -0.0225 0.4258 0.2486
2.750 0.4112 0.02753 0.02061 -0.0216 0.4229 0.2683
3.000 0.4324 0.02764 0.02111 -0.0220 0.4196 0.3800
3.250 0.4507 0.02808 0.02175 -0.0218 0.4183 0.4244
3.500 0.4691 0.02854 0.02232 -0.0215 0.4167 0.4553
3.750 0.4861 0.02907 0.02294 -0.0210 0.4148 0.4757
4.000 0.5007 0.02974 0.02369 -0.0203 0.4126 0.4962
4.250 0.5151 0.03040 0.02441 -0.0196 0.4099 0.5183
4.500 0.5290 0.03103 0.02513 -0.0188 0.4073 0.5478
4.750 0.5437 0.03159 0.02576 -0.0180 0.4043 0.5759
5.000 0.5604 0.03193 0.02627 -0.0174 0.4023 0.6227
5.250 0.5669 0.03250 0.02721 -0.0152 0.4009 0.7084
5.500 0.7344 0.03528 0.03081 -0.0463 0.3988 0.9405
5.750 0.7266 0.03603 0.03157 -0.0411 0.3966 0.9533
6.000 0.7517 0.03710 0.03262 -0.0427 0.3944 0.9588
6.250 0.7741 0.03833 0.03382 -0.0440 0.3917 0.9647
6.500 0.7791 0.03934 0.03480 -0.0416 0.3893 0.9700
6.750 0.7989 0.04019 0.03559 -0.0419 0.3862 0.9731
7.000 0.8407 0.04172 0.03715 -0.0476 0.3850 0.9750
7.250 0.8855 0.04313 0.03856 -0.0537 0.3834 0.9776
7.500 0.9217 0.04440 0.03984 -0.0580 0.3815 0.9803
7.750 0.9490 0.04553 0.04096 -0.0604 0.3796 0.9826
8.000 0.9749 0.04676 0.04218 -0.0626 0.3776 0.9855
8.250 0.9867 0.04829 0.04370 -0.0625 0.3752 0.9876
8.500 1.0085 0.04970 0.04508 -0.0641 0.3727 0.9900
8.750 1.0441 0.05044 0.04577 -0.0680 0.3699 0.9916
9.000 1.0676 0.05173 0.04710 -0.0703 0.3686 0.9931
9.250 1.0953 0.05290 0.04829 -0.0731 0.3672 0.9953
9.500 1.1194 0.05429 0.04969 -0.0756 0.3653 0.9974
9.750 1.1452 0.05577 0.05119 -0.0785 0.3635 0.9994
10.000 1.1595 0.05699 0.05241 -0.0788 0.3615 0.9998
10.250 1.1698 0.05822 0.05362 -0.0784 0.3593 1.0000
10.500 1.1784 0.05935 0.05473 -0.0776 0.3569 1.0000
10.750 1.1938 0.05991 0.05524 -0.0773 0.3544 1.0000
11.000 1.1985 0.06144 0.05681 -0.0763 0.3532 1.0000
11.250 1.2058 0.06278 0.05820 -0.0756 0.3519 1.0000
11.500 1.2148 0.06399 0.05943 -0.0750 0.3504 1.0000
11.750 1.2229 0.06529 0.06075 -0.0743 0.3489 1.0000
12.000 1.2269 0.06693 0.06241 -0.0733 0.3469 1.0000
12.250 1.2348 0.06823 0.06371 -0.0727 0.3451 1.0000
12.500 1.2437 0.06944 0.06492 -0.0722 0.3433 1.0000
12.750 1.2544 0.07047 0.06592 -0.0718 0.3412 1.0000
13.000 1.2727 0.07081 0.06622 -0.0720 0.3388 1.0000
13.250 1.2719 0.07293 0.06840 -0.0709 0.3375 1.0000
13.500 1.2776 0.07447 0.06999 -0.0703 0.3364 1.0000
13.750 1.2829 0.07606 0.07161 -0.0697 0.3347 1.0000
14.000 1.2859 0.07787 0.07345 -0.0689 0.3328 1.0000
14.250 1.2891 0.07965 0.07526 -0.0682 0.3310 1.0000
14.500 1.2978 0.08093 0.07655 -0.0679 0.3295 1.0000
14.750 1.3066 0.08216 0.07777 -0.0676 0.3277 1.0000
15.000 1.3198 0.08298 0.07856 -0.0676 0.3257 1.0000
15.250 1.3381 0.08329 0.07885 -0.0680 0.3241 1.0000
15.500 1.3385 0.08533 0.08094 -0.0672 0.3226 1.0000
15.750 1.3368 0.08758 0.08325 -0.0663 0.3213 1.0000
16.000 1.3307 0.09029 0.08603 -0.0652 0.3183 1.0000
16.250 1.3317 0.09228 0.08806 -0.0646 0.3169 1.0000
16.500 1.3342 0.09417 0.08996 -0.0641 0.3146 1.0000
16.750 1.3417 0.09553 0.09129 -0.0639 0.3122 1.0000
17.000 1.3580 0.09599 0.09171 -0.0643 0.3097 1.0000
17.250 1.3739 0.09649 0.09220 -0.0646 0.3085 1.0000
17.500 1.3620 0.09975 0.09557 -0.0633 0.3072 1.0000
17.750 1.3545 0.10260 0.09849 -0.0624 0.3049 1.0000
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